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Development Status of the Fission Power System Technology Demonstration UnitThis paper summarizes the progress that has been made in the development of the Fission Power System Technology Demonstration Unit (TDU). The reactor simulator core and Annular Linear Induction Pump have been fabricated and assembled into a test loop at the NASA Marshall Space Flight Center. A 12 kWe Power Conversion Unit (PCU) is being developed consisting of two 6 kWe free-piston Stirling engines. The two 6 kWe engines have been fabricated by Sunpower Inc. and are currently being tested separately prior to integration into the PCU. The Facility Cooling System (FCS) used to reject convertor waste heat has been assembled and tested at the NASA Glenn Research Center (GRC). The structural elements, including a Buildup Assembly Platform (BAP) and Upper Truss Structure (UTS) have been fabricated, and will be used to test cold-end components in thermal vacuum prior to TDU testing. Once all components have been fully tested at the subsystem level, they will be assembled into an end-to-end system and tested in thermal vacuum at NASA GRC.
Document ID
20130010732
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Briggs, Maxwell H.
(NASA Glenn Research Center Cleveland, OH, United States)
Gibson, Marc A.
(NASA Glenn Research Center Cleveland, OH, United States)
Geng, Steven M
(NASA Glenn Research Center Cleveland, OH, United States)
Pearson, Jon Boise
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Godfroy, Thomas
(Maximum Technology Corp. Huntsville, AL, United States)
Date Acquired
August 27, 2013
Publication Date
July 30, 2012
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-18230-1
Meeting Information
Meeting: International Energy Conversion Engineering
Location: Atlanta, GA
Country: United States
Start Date: July 30, 2012
End Date: August 1, 2012
Funding Number(s)
WBS: WBS 887359.01 .04
Distribution Limits
Public
Copyright
Public Use Permitted.
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